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Final rule 2026-08106

Airworthiness Directives; Pratt & Whitney Engines

The FAA is adopting a new airworthiness directive (AD) for certain Pratt & Whitney (PW) Model F117-PW-100, PW2037, PW2037D, PW2037M, PW2040, and PW2040D engines. This AD was prompted by an updated analysis of an event involving an International Aero Engines, LLC (IAE LLC) Model PW1127GA-JM engine, which experienced a high- pressure compressor (HPC) 7th-stage integrally bladed rotor (IBR-7) separation that resulted in an engine shutdown and aborted takeoff. This AD requires repetitive angled ultrasonic inspections (AUSIs) of certain high-pressure turbine (HPT) 1st-stage disks and turbine hubs for any crack indications, and if necessary, removal from service and replacement, and removal from service of certain HPT lenticular seal assemblies. The FAA is issuing this AD to address the unsafe condition on these products.

Source: FederalRegister.gov API v1Recently refreshed. Last successful refresh: 2026-07-31 22:49:02 UTC.

Source-supplied record

Document details

Document number
2026-08106
Published
Apr 24, 2026
Effective
May 29, 2026
Comments close
Not supplied
Federal Register citation
91 FR 21945

Docket identifiers

  • Docket No. FAA-2025-0918
  • Project Identifier AD-2024-00526-E
  • Amendment 39-23301
  • AD 2026-07-06

CFR references

  • Title 14, part 39